Abstract
Nomenclature Ab = base area, 7rr& CA = axial force coefficient Cm = pitching moment coefficient, Moment/qmA bDb MOO = freestream Mach number pQ' = normal shock stagnation pressure rn/n = nose-to-base radius ratio Re^/m. = freestream unit Reynolds number, in. ZB = axial distance measured from center of spherical nose, distance/rn, a. = angle of attack, deg j = specific heats ratio OB = polar angle measured from most windward streamline, deg Bc = cone half-angle, deg
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